Date:
October 22nd 2009
ISS TRAJECTORY DATA
Lift off time (UTC) : N/A Area (sq ft) : 14692 74 Drag Coefficient (Cd) : 2 00 Monthly MSFC 50% solar flux (F10 7-jansky) : 72 1 Monthly MSFC 50% earth geomagnetic index (Kp) : 1 39 ET - UTC (sec) : 66 18 UT1 - UTC (sec) : 0 00
Maneuvers contained within the current ephemeris are as follows:
IMPULSIVE TIG (GMT) M50 DVx(FPS) LVLH DVx(FPS) DVmag(FPS) IMPULSIVE TIG (MET) M50 DVy(FPS) LVLH DVy(FPS) Invar Sph HA DT M50 DVz(FPS) LVLH DVz(FPS) Invar Sph HP
There are no maneuvers
Coasting Arc #1 (Orbit 2584)
---------------------------------------
Vector Time (GMT): 2009/294/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6268645
13 A = 6726431
09 meter
Y = -21404
02 meter E =
0001780
Z = -2439129
93 I = 51
75843
XDOT = 2105
469855 Wp = 239
46988
YDOT = 5105
662053 meter/sec RA = 17
66165 deg
ZDOT = 5362
551579 TA = 93
03388
MA = 93
01352
Ha = 187
985 n
mi
Hp = 183
966
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20566421
02 X = 6280267
74
Y = -70223
15 feet Y = 48760
68 meter
Z = -8002394
77 Z = -2408647
79
XDOT = 6907
709498 XDOT = 2022
169959
YDOT = 16750
859753 feet/sec YDOT = 5128
740850 meter/sec
ZDOT = 17593
673161 ZDOT = 5372
577938
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -17941780
11 X = -5468654
58
Y = 10148127
49 feet Y = 3093149
26 meter
Z = -7882192
71 Z = -2402492
34
XDOT = -13391
564961 XDOT = -4081
749000
YDOT = -9970
284170 feet/sec YDOT = -3038
942615 meter/sec
ZDOT = 17633
386863 ZDOT = 5374
656316
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09294
50478377
00001200 00000-0 20000-3 0 9005
2 25544 51
6446 18
1727 0007299 229
9225 130
1300 15
75135577 25856
Satellite: ISS
Catalog Number: 25544
Epoch time: 09294
50478377 = yrday
fracday
Element set: 900
Inclination: 51
6446 deg
RA of node: 18
1727 deg
Eccentricity:
0007299
Arg of perigee: 229
9225 deg
Mean anomaly: 130
1300 deg
Mean motion: 15
75135577 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2585
Checksum: 303
Coasting Arc #2 (Orbit 2600)
---------------------------------------
Vector Time (GMT): 2009/295/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1727777
56 A = 6718511
75 meter
Y = -4314295
71 meter E =
0005951
Z = -4856584
35 I = 51
70258
XDOT = 7322
303281 Wp = 97
34679
YDOT = -278
274101 meter/sec RA = 12
56391 deg
ZDOT = -2360
983429 TA = 149
66797
MA = 149
63352
Ha = 187
754 n
mi
Hp = 183
929
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -5668561
56 X = -1655812
98
Y = -14154513
48 feet Y = -4333214
26 meter
Z = -15933675
70 Z = -4864803
37
XDOT = 24023
304729 XDOT = 7336
340275
YDOT = -912
972772 feet/sec YDOT = -196
313259 meter/sec
ZDOT = -7746
008626 ZDOT = -2325
376753
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11952534
66 X = 3643132
56
Y = 9411760
04 feet Y = 2868704
46 meter
Z = -15966231
60 Z = -4866507
39
XDOT = -19637
104010 XDOT = -5985
389302
YDOT = 12053
835667 feet/sec YDOT = 3674
009111 meter/sec
ZDOT = -7605
604976 ZDOT = -2318
188397
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09295
51985538
00001200 00000-0 20000-3 0 9010
2 25544 51
6438 12
9513 0007285 233
3250 126
7244 15
75179601 26017
Satellite: ISS
Catalog Number: 25544
Epoch time: 09295
51985538 = yrday
fracday
Element set: 901
Inclination: 51
6438 deg
RA of node: 12
9513 deg
Eccentricity:
0007285
Arg of perigee: 233
3250 deg
Mean anomaly: 126
7244 deg
Mean motion: 15
75179601 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2601
Checksum: 289
Coasting Arc #3 (Orbit 2616)
---------------------------------------
Vector Time (GMT): 2009/296/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6491770
68 A = 6727501
42 meter
Y = 484645
26 meter E =
0012101
Z = 1666079
84 I = 51
70363
XDOT = -1833
967058 Wp = 146
05566
YDOT = -4806
583264 meter/sec RA = 7
39010 deg
ZDOT = -5737
690198 TA = 15
52780
MA = 15
49071
Ha = 187
496 n
mi
Hp = 184
047
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21298460
25 X = -6504801
26
Y = 1590043
49 feet Y = 411977
56 meter
Z = 5466141
22 Z = 1634510
55
XDOT = -6016
952291 XDOT = -1752
209488
YDOT = -15769
630130 feet/sec YDOT = -4826
634505 meter/sec
ZDOT = -18824
442906 ZDOT = -5746
401301
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 17406290
36 X = 5305437
30
Y = -12430568
52 feet Y = -3788837
29 meter
Z = 5341663
53 Z = 1628139
04
XDOT = 12327
917387 XDOT = 3757
549220
YDOT = 9143
971691 feet/sec YDOT = 2787
082571 meter/sec
ZDOT = -18858
953645 ZDOT = -5748
209071
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09296
53490338
00001200 00000-0 20000-3 0 9023
2 25544 51
6438 7
7298 0007038 237
6244 122
4239 15
75239950 26173
Satellite: ISS
Catalog Number: 25544
Epoch time: 09296
53490338 = yrday
fracday
Element set: 902
Inclination: 51
6438 deg
RA of node: 7
7298 deg
Eccentricity:
0007038
Arg of perigee: 237
6244 deg
Mean anomaly: 122
4239 deg
Mean motion: 15
75239950 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2617
Checksum: 308
Coasting Arc #4 (Orbit 2632)
---------------------------------------
Vector Time (GMT): 2009/297/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 1436093
52 A = 6717079
20 meter
Y = 4110909
66 meter E =
0006503
Z = 5117892
87 I = 51
63931
XDOT = -7519
423476 Wp = 203
63157
YDOT = 836
369588 meter/sec RA = 2
27447 deg
ZDOT = 1432
935330 TA = 232
61031
MA = 232
66953
Ha = 187
135 n
mi
Hp = 184
165
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 4711592
93 X = 1365155
66
Y = 13487236
40 feet Y = 4126572
18 meter
Z = 16790987
09 Z = 5124697
28
XDOT = -24670
024528 XDOT = -7535
178100
YDOT = 2743
994711 feet/sec YDOT = 752
194851 meter/sec
ZDOT = 4701
231397 ZDOT = 1396
367098
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -11099575
36 X = -3383150
57
Y = -8944143
31 feet Y = -2726174
88 meter
Z = 16817955
54 Z = 5126112
85
XDOT = 18769
308914 XDOT = 5720
885357
YDOT = -14691
535497 feet/sec YDOT = -4477
980020 meter/sec
ZDOT = 4557
050203 ZDOT = 1388
988902
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09297
54992674
00001200 00000-0 20000-3 0 9036
2 25544 51
6439 2
5074 0007113 242
1092 117
9352 15
75285967 26337
Satellite: ISS
Catalog Number: 25544
Epoch time: 09297
54992674 = yrday
fracday
Element set: 903
Inclination: 51
6439 deg
RA of node: 2
5074 deg
Eccentricity:
0007113
Arg of perigee: 242
1092 deg
Mean anomaly: 117
9352 deg
Mean motion: 15
75285967 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2633
Checksum: 305
Coasting Arc #5 (Orbit 2647)
---------------------------------------
Vector Time (GMT): 2009/298/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6603475
78 A = 6728327
35 meter
Y = -977342
50 meter E =
0005482
Z = -812805
48 I = 51
64624
XDOT = 1422
695416 Wp = 2
50464
YDOT = 4655
772657 meter/sec RA = 357
10994 deg
ZDOT = 5967
041829 TA = 348
62898
MA = 348
64136
Ha = 186
864 n
mi
Hp = 184
310
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 21664946
78 X = 6617862
32
Y = -3206504
28 feet Y = -903418
10 meter
Z = -2666684
63 Z = -780690
37
XDOT = 4667
635878 XDOT = 1341
540769
YDOT = 15274
844674 feet/sec YDOT = 4671
228284 meter/sec
ZDOT = 19576
908888 ZDOT = 5973
756285
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -16375228
10 X = -4991169
53
Y = 14565807
54 feet Y = 4439658
14 meter
Z = -2540069
02 Z = -774213
04
XDOT = -11119
154205 XDOT = -3389
118202
YDOT = -9085
974290 feet/sec YDOT = -2769
404964 meter/sec
ZDOT = 19603
541097 ZDOT = 5975
159326
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09298
50149165
00001200 00000-0 20000-3 0 9043
2 25544 51
6433 357
6117 0006880 247
6585 112
3850 15
75260176 26483
Satellite: ISS
Catalog Number: 25544
Epoch time: 09298
50149165 = yrday
fracday
Element set: 904
Inclination: 51
6433 deg
RA of node: 357
6117 deg
Eccentricity:
0006880
Arg of perigee: 247
6585 deg
Mean anomaly: 112
3850 deg
Mean motion: 15
75260176 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2648
Checksum: 308
Coasting Arc #6 (Orbit 2663)
---------------------------------------
Vector Time (GMT): 2009/299/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -1026543
36 A = 6716382
25 meter
Y = -4064672
46 meter E =
0008644
Z = -5254543
41 I = 51
57662
XDOT = 7559
994624 Wp = 99
89398
YDOT = -1389
686576 meter/sec RA = 351
97340 deg
ZDOT = -403
966782 TA = 166
27672
MA = 166
25321
Ha = 186
611 n
mi
Hp = 184
243
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -3367924
42 X = -955489
20
Y = -13335539
56 feet Y = -4075754
63 meter
Z = -17239315
65 Z = -5259357
80
XDOT = 24803
131969 XDOT = 7576
934887
YDOT = -4559
339161 feet/sec YDOT = -1305
051546 meter/sec
ZDOT = -1325
350335 ZDOT = -367
198630
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10202206
44 X = 3109632
52
Y = 9188845
34 feet Y = 2800760
06 meter
Z = -17258436
76 Z = -5260371
52
XDOT = -17279
526037 XDOT = -5266
799536
YDOT = 16980
559031 feet/sec YDOT = 5175
674393 meter/sec
ZDOT = -1180
400526 ZDOT = -359
786080
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09299
51647138
00001200 00000-0 20000-3 0 9059
2 25544 51
6433 352
3891 0006871 250
6796 109
3625 15
75319234 26646
Satellite: ISS
Catalog Number: 25544
Epoch time: 09299
51647138 = yrday
fracday
Element set: 905
Inclination: 51
6433 deg
RA of node: 352
3891 deg
Eccentricity:
0006871
Arg of perigee: 250
6796 deg
Mean anomaly: 109
3625 deg
Mean motion: 15
75319234 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2664
Checksum: 317
Coasting Arc #7 (Orbit 2679)
---------------------------------------
Vector Time (GMT): 2009/300/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6564178
19 A = 6728214
55 meter
Y = 1439978
37 meter E =
0010468
Z = -119101
74 I = 51
58827
XDOT = -923
039471 Wp = 169
44808
YDOT = -4699
198707 meter/sec RA = 346
82187 deg
ZDOT = -6035
743658 TA = 11
84775
MA = 11
82314
Ha = 186
187 n
mi
Hp = 184
162
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -21536017
69 X = -6579213
83
Y = 4724338
49 feet Y = 1366489
79 meter
Z = -390753
76 Z = -151027
58
XDOT = -3028
344722 XDOT = -841
102600
YDOT = -15417
318592 feet/sec YDOT = -4709
062691 meter/sec
ZDOT = -19802
308590 ZDOT = -6040
028712
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 14869447
26 X = 4532207
53
Y = -16275895
68 feet Y = -4960893
00 meter
Z = -516602
80 Z = -157460
53
XDOT = 10082
589882 XDOT = 3073
173396
YDOT = 9833
043959 feet/sec YDOT = 2997
111799 meter/sec
ZDOT = -19819
365207 ZDOT = -6040
942515
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09300
53142725
00001200 00000-0 20000-3 0 9067
2 25544 51
6439 347
1667 0006660 255
3818 104
6608 15
75391101 26808
Satellite: ISS
Catalog Number: 25544
Epoch time: 09300
53142725 = yrday
fracday
Element set: 906
Inclination: 51
6439 deg
RA of node: 347
1667 deg
Eccentricity:
0006660
Arg of perigee: 255
3818 deg
Mean anomaly: 104
6608 deg
Mean motion: 15
75391101 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2680
Checksum: 287
Coasting Arc #8 (Orbit 2695)
---------------------------------------
Vector Time (GMT): 2009/301/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 582717
09 A = 6716210
56 meter
Y = 4182872
38 meter E =
0003821
Z = 5225504
39 I = 51
51851
XDOT = -7433
773644 Wp = 272
40066
YDOT = 1890
533307 meter/sec RA = 341
66268 deg
ZDOT = -684
621622 TA = 184
11877
MA = 184
12191
Ha = 185
884 n
mi
Hp = 184
092
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1911801
47 X = 510515
16
Y = 13723334
59 feet Y = 4188985
17 meter
Z = 17144043
27 Z = 5228159
74
XDOT = -24389
021141 XDOT = -7451
035588
YDOT = 6202
537098 feet/sec YDOT = 1807
307924 meter/sec
ZDOT = -2246
133930 ZDOT = -720
777543
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9566640
14 X = -2915911
91
Y = -10005010
63 feet Y = -3049527
24 meter
Z = 17154657
54 Z = 5228739
62
XDOT = 15278
329265 XDOT = 4656
834760
YDOT = -18702
963266 feet/sec YDOT = -5700
663204 meter/sec
ZDOT = -2388
643443 ZDOT = -728
058521
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09301
54635968
00001200 00000-0 20000-3 0 9076
2 25544 51
6432 341
9444 0006655 259
2482 100
7933 15
75426813 26964
Satellite: ISS
Catalog Number: 25544
Epoch time: 09301
54635968 = yrday
fracday
Element set: 907
Inclination: 51
6432 deg
RA of node: 341
9444 deg
Eccentricity:
0006655
Arg of perigee: 259
2482 deg
Mean anomaly: 100
7933 deg
Mean motion: 15
75426813 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2696
Checksum: 312
Coasting Arc #9 (Orbit 2711)
---------------------------------------
Vector Time (GMT): 2009/302/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 6376829
63 A = 6727622
43 meter
Y = -1830569
38 meter E =
0008687
Z = 1083772
49 I = 51
52877
XDOT = 410
523374 Wp = 36
63165
YDOT = 4934
231692 meter/sec RA = 336
52464 deg
ZDOT = 5901
421133 TA = 335
25179
MA = 335
29344
Ha = 185
702 n
mi
Hp = 183
935
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 20921357
07 X = 6391560
55
Y = -6005805
07 feet Y = -1759177
50 meter
Z = 3555684
01 Z = 1114787
66
XDOT = 1346
861462 XDOT = 326
648767
YDOT = 16188
424186 feet/sec YDOT = 4938
353723 meter/sec
ZDOT = 19361
617889 ZDOT = 5903
211525
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -13021945
00 X = -3969088
84
Y = 17416016
46 feet Y = 5308401
82 meter
Z = 3677918
41 Z = 1121029
53
XDOT = -9496
733921 XDOT = -2894
604499
YDOT = -11202
650589 feet/sec YDOT = -3414
567900 meter/sec
ZDOT = 19368
848594 ZDOT = 5903
625051
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09302
56127165
00001200 00000-0 20000-3 0 9085
2 25544 51
6432 336
7212 0006428 265
1363 94
9067 15
75412067 27128
Satellite: ISS
Catalog Number: 25544
Epoch time: 09302
56127165 = yrday
fracday
Element set: 908
Inclination: 51
6432 deg
RA of node: 336
7212 deg
Eccentricity:
0006428
Arg of perigee: 265
1363 deg
Mean anomaly: 94
9067 deg
Mean motion: 15
75412067 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2712
Checksum: 285
Coasting Arc #10 (Orbit 2726)
---------------------------------------
Vector Time (GMT): 2009/303/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -148463
25 A = 6717052
66 meter
Y = -4471583
82 meter E =
0007207
Z = -5016541
13 I = 51
46730
XDOT = 7133
619810 Wp = 117
82717
YDOT = -2261
819146 meter/sec RA = 331
34223 deg
ZDOT = 1803
653627 TA = 169
60941
MA = 169
59451
Ha = 185
493 n
mi
Hp = 183
885
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -487084
16 X = -74080
10
Y = -14670550
59 feet Y = -4472828
38 meter
Z = -16458468
27 Z = -5017081
47
XDOT = 23404
264469 XDOT = 7149
619621
YDOT = -7420
666491 feet/sec YDOT = -2181
957252 meter/sec
ZDOT = 5917
498777 ZDOT = 1838
348629
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 9373520
38 X = 2857049
01
Y = 11292659
47 feet Y = 3442002
61 meter
Z = -16460754
57 Z = -5017237
99
XDOT = -12963
840918 XDOT = -3951
378712
YDOT = 19592
049255 feet/sec YDOT = 5971
656613 meter/sec
ZDOT = 6054
222006 ZDOT = 1845
326867
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09303
51272687
00001200 00000-0 20000-3 0 9092
2 25544 51
6440 331
8247 0006555 268
0113 92
0300 15
75464805 27279
Satellite: ISS
Catalog Number: 25544
Epoch time: 09303
51272687 = yrday
fracday
Element set: 909
Inclination: 51
6440 deg
RA of node: 331
8247 deg
Eccentricity:
0006555
Arg of perigee: 268
0113 deg
Mean anomaly: 92
0300 deg
Mean motion: 15
75464805 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2727
Checksum: 283
Coasting Arc #11 (Orbit 2742)
---------------------------------------
Vector Time (GMT): 2009/304/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -6052921
60 A = 6725951
30 meter
Y = 2072670
05 meter E =
0005186
Z = -2063423
02 I = 51
47152
XDOT = 58
079194 Wp = 205
08719
YDOT = -5348
346379 meter/sec RA = 326
21724 deg
ZDOT = -5542
235427 TA = 358
01437
MA = 358
01643
Ha = 185
423 n
mi
Hp = 183
755
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -19858666
67 X = -6065624
64
Y = 6800098
59 feet Y = 2004911
60 meter
Z = -6769760
57 Z = -2092859
96
XDOT = 190
548537 XDOT = 144
805022
YDOT = -17547
068174 feet/sec YDOT = -5347
212225 meter/sec
ZDOT = -18183
187096 ZDOT = -5541
742383
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 11075079
60 X = 3375684
26
Y = -17786698
78 feet Y = -5421385
79 meter
Z = -6885753
35 Z = -2098777
62
XDOT = 9552
340762 XDOT = 2911
553464
YDOT = 12986
995626 feet/sec YDOT = 3958
436267 meter/sec
ZDOT = -18181
428851 ZDOT = -5541
699514
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09304
52759140
00001200 00000-0 20000-3 0 9100
2 25544 51
6433 326
6015 0006451 271
7303 88
3123 15
75514788 27438
Satellite: ISS
Catalog Number: 25544
Epoch time: 09304
52759140 = yrday
fracday
Element set: 910
Inclination: 51
6433 deg
RA of node: 326
6015 deg
Eccentricity:
0006451
Arg of perigee: 271
7303 deg
Mean anomaly: 88
3123 deg
Mean motion: 15
75514788 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2743
Checksum: 280
Coasting Arc #12 (Orbit 2758)
---------------------------------------
Vector Time (GMT): 2009/305/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -216530
84 A = 6718491
99 meter
Y = 4894313
22 meter E =
0004464
Z = 4598546
07 I = 51
42128
XDOT = -6701
382917 Wp = 14
98211
YDOT = 2439
988165 meter/sec RA = 321
01493 deg
ZDOT = -2907
591858 TA = 103
91920
MA = 103
86954
Ha = 185
516 n
mi
Hp = 183
723
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -710403
03 X = -293583
49
Y = 16057458
06 feet Y = 4891461
12 meter
Z = 15087093
39 Z = 4597306
85
XDOT = -21986
164426 XDOT = -6714
044177
YDOT = 8005
210516 feet/sec YDOT = 2364
978492 meter/sec
ZDOT = -9539
343367 ZDOT = -2940
179107
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9741148
98 X = -2969102
21
Y = -12790581
37 feet Y = -3898569
20 meter
Z = 15082375
92 Z = 4597108
18
XDOT = 10671
981130 XDOT = 3252
819848
YDOT = -19546
513747 feet/sec YDOT = -5957
777390 meter/sec
ZDOT = -9667
741448 ZDOT = -2946
727593
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09305
54243207
00001200 00000-0 20000-3 0 9116
2 25544 51
6421 321
3779 0006402 276
6418 83
4017 15
75575250 27597
Satellite: ISS
Catalog Number: 25544
Epoch time: 09305
54243207 = yrday
fracday
Element set: 911
Inclination: 51
6421 deg
RA of node: 321
3779 deg
Eccentricity:
0006402
Arg of perigee: 276
6418 deg
Mean anomaly: 83
4017 deg
Mean motion: 15
75575250 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2759
Checksum: 285
Coasting Arc #13 (Orbit 2774)
---------------------------------------
Vector Time (GMT): 2009/306/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 5627068
19 A = 6723674
52 meter
Y = -2126032
74 meter E =
0007349
Z = 2994821
79 I = 51
41612
XDOT = -409
905906 Wp = 68
99605
YDOT = 5892
569754 meter/sec RA = 315
89827 deg
ZDOT = 4946
195707 TA = 325
76476
MA = 325
81211
Ha = 185
581 n
mi
Hp = 183
679
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 18461509
79 X = 5635874
80
Y = -6975173
04 feet Y = -2063058
32 meter
Z = 9825530
81 Z = 3022180
47
XDOT = -1344
835651 XDOT = -499
795786
YDOT = 19332
577932 feet/sec YDOT = 5887
483319 meter/sec
ZDOT = 16227
676204 ZDOT = 4943
985989
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = -9275726
86 X = -2827241
55
Y = 17358323
32 feet Y = 5290816
95 meter
Z = 9933324
80 Z = 3027677
40
XDOT = -10365
089506 XDOT = -3159
279281
YDOT = -14833
471869 feet/sec YDOT = -4521
242226 meter/sec
ZDOT = 16219
163723 ZDOT = 4943
601103
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09306
55725046
00001200 00000-0 20000-3 0 9125
2 25544 51
6417 316
1540 0006387 281
0804 78
9642 15
75587537 27753
Satellite: ISS
Catalog Number: 25544
Epoch time: 09306
55725046 = yrday
fracday
Element set: 912
Inclination: 51
6417 deg
RA of node: 316
1540 deg
Eccentricity:
0006387
Arg of perigee: 281
0804 deg
Mean anomaly: 78
9642 deg
Mean motion: 15
75587537 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2775
Checksum: 310
Coasting Arc #14 (Orbit 2789)
---------------------------------------
Vector Time (GMT): 2009/307/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = 456518
78 A = 6720728
40 meter
Y = -5400803
83 meter E =
0000666
Z = -3974556
11 I = 51
38586
XDOT = 6181
215045 Wp = 134
95134
YDOT = -2371
886222 meter/sec RA = 310
68304 deg
ZDOT = 3932
938430 TA = 175
86460
MA = 175
86405
Ha = 185
880 n
mi
Hp = 183
697
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = 1497765
03 X = 536185
96
Y = -17719172
66 feet Y = -5395253
19 meter
Z = -13039882
27 Z = -3972144
93
XDOT = 20279
576920 XDOT = 6188
172285
YDOT = -7781
778942 feet/sec YDOT = -2302
725467 meter/sec
ZDOT = 12903
341306 ZDOT = 3962
984681
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 10714380
24 X = 3265743
10
Y = 14200618
95 feet Y = 4328348
66 meter
Z = -13030555
90 Z = -3971713
44
XDOT = -8734
784914 XDOT = -2662
362442
YDOT = 18539
389516 feet/sec YDOT = 5650
805924 meter/sec
ZDOT = 13021
725719 ZDOT = 3969
021999
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09307
50862017
00001200 00000-0 20000-3 0 9132
2 25544 51
6420 311
2568 0006439 285
2088 74
8364 15
75608434 27904
Satellite: ISS
Catalog Number: 25544
Epoch time: 09307
50862017 = yrday
fracday
Element set: 913
Inclination: 51
6420 deg
RA of node: 311
2568 deg
Eccentricity:
0006439
Arg of perigee: 285
2088 deg
Mean anomaly: 74
8364 deg
Mean motion: 15
75608434 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2790
Checksum: 298
Coasting Arc #15 (Orbit 2805)
---------------------------------------
Vector Time (GMT): 2009/308/12:00:00
000
Vector Time (MET): N/A
Weight (LBS) : 745169
1
M50 Cartesian M50 Keplerian
----------------------------------- --------------------------------
X = -5163744
63 A = 6720952
57 meter
Y = 1942927
68 meter E =
0003894
Z = -3841530
88 I = 51
36745
XDOT = 611
381297 Wp = 3
19352
YDOT = -6487
949385 meter/sec RA = 305
56743 deg
ZDOT = -4099
582705 TA = 223
81790
MA = 223
84881
Ha = 186
037 n
mi
Hp = 183
471
M50 Cartesian J2K Cartesian
----------------------------------- --------------------------------
X = -16941419
39 X = -5166424
91
Y = 6374434
64 feet Y = 1885168
89 meter
Z = -12603447
78 Z = -3866623
59
XDOT = 2005
844150 XDOT = 703
800932
YDOT = -21285
923178 feet/sec YDOT = -6480
595567 meter/sec
ZDOT = -13450
074492 ZDOT = -4096
388411
TDR Cartesian TDR Cartesian
----------------------------------- --------------------------------
X = 7961817
70 X = 2426762
03
Y = -16178767
51 feet Y = -4931288
34 meter
Z = -12702320
44 Z = -3871667
27
XDOT = 11841
437368 XDOT = 3609
270110
YDOT = 16386
880012 feet/sec YDOT = 4994
721028 meter/sec
ZDOT = -13437
693975 ZDOT = -4095
809124
The mean element set is posted at the UTC for which position is
just north of the next ascending node relative to the above
vector time
TWO LINE MEAN ELEMENT SET
ISS
1 25544U 98067A 09308
52339211
00001200 00000-0 20000-3 0 9141
2 25544 51
6409 306
0321 0006398 288
8869 71
1601 15
75652237 28062
Satellite: ISS
Catalog Number: 25544
Epoch time: 09308
52339211 = yrday
fracday
Element set: 914
Inclination: 51
6409 deg
RA of node: 306
0321 deg
Eccentricity:
0006398
Arg of perigee: 288
8869 deg
Mean anomaly: 71
1601 deg
Mean motion: 15
75652237 rev/day
Decay rate: 1
20000E-05 rev/day^2
Epoch rev: 2806
Checksum: 295
INTERNATIONAL SPACE STATION ORBITAL DATA:
The state vectors and 2-Line Elements (TLEs) are obtained from various sources at different times depending upon availability The data normally contains past, current and predicted orbital data Careful attention to the orbit # / epoch times! These sources include:
NASA Orbital Flight Dynamics DOD C-Band Radar Network Goddard Space Flight Center (GSFC) NASA Johnson Space Center (JSC) DoD/ USSTRATCOM/ US Space Command with permission
By receiving this email, you agree not to transfer any data or information received under this agreement, including the analysis of tracking data, to any other entity without the express approval of the Aus-City Forum Admins and/ or DoD/ USSTRATCOM/ US Space Command
David Cottle
Director Of Engineering
IDB Communications
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